Cessna 560 - Page 14

Aug 13/2004 560-34-114
Revision 2 - Jan 2/2007 Page 10
Citation SERVICE BULLETIN
SB560-34-114
to match the 9690567-1 and 9690555-1 Cable Assemblies. (Refer to Cessna Engineering
Drawings 9690567 and 9690555.)
(7) (Airplanes that will have the 066-01146-1211 TCAS II Computer installed at location option D
and the Primus Communication Units installed at location option 2.) Change the existing wiring
to match the 9690567-1 and 9690558-1 Cable Assemblies. (Refer to Cessna Engineering
Drawings 9690567 and 9690558.)
B. (Airplanes that have the TCAS I system installed and are upgrading to the TCAS II system.) Install
the appropriate TCAS II and Primus II cable assemblies.
(1) (Airplanes that will have the 066-01146-1211 TCAS II Computer installed at location option B
and the Primus Communication Units installed at location option 1.) Change the existing wiring
to match the 9690565-1 and 9690555-1 Cable Assemblies. (Refer to Cessna Engineering
Drawings 9690565 and 9690555.)
(2) (Airplanes that will have the 066-01146-1211 TCAS II Computer installed at location option B
and the Primus Communication Units installed at location option 2.) Change the existing wiring
to match the 9690565-1 and 9690558-1 Cable Assemblies. (Refer to Cessna Engineering
Drawings 9690565 and 9690558.)
(3) (Airplanes that will have the 066-01146-1211 TCAS II Computer installed at location option C
and the Primus Communication Units installed at location option 2.) Change the existing wiring
to match the 9690577-1 and 9690558-1 Cable Assemblies. (Refer to Cessna Engineering
Drawings 9690577 and 9690558.)
(4) (Airplanes that will have the 066-01146-1211 TCAS II Computer installed at location option D
and the Primus Communication Units installed at location option 1.) Change the existing wiring
to match the 9690576-1 and 9690555-1 Cable Assemblies. (Refer to Cessna Engineering
Drawings 9690576 and 9690555.)
(5) (Airplanes that will have the 066-01146-1211 TCAS II Computer installed at location option D
and the Primus Communication Units installed at location option 2.) Change the existing wiring
to match the 9690576-1 and 9690558-1 Cable Assemblies. (Refer to Cessna Engineering
Drawings 9690576 and 9690558.)
C. Use the applicable subkit and Cessna Engineering Drawing to locate and install the 066-01146-1211
TCAS II Computer. (Refer to Cessna Engineering Drawing 9690551-1, 9690560-1, 9690559-2,
9690545-1, 9690554-1, 9690553-1 or 9690468-1.)
(1) Use the 9622012, 9656082 and 9690446 drawings to build installations shown in the 9690560,
9690559 and 9690554 drawings.
D. Locate and install the test port. (Refer to Cessna Engineering Drawing 9690476-1.)
E. Install the 9690574 Feed Thru Plate Installation. (Refer to Cessna Engineering Drawing 9690574.)
(1) Airplanes installing the TCAS II Computer at location option A, use the 9690574-1 installation.
(2) Airplanes installing the TCAS II Computer at location options B through D, use the 9690574-2
installation.
F. (Airplanes that do not have the TCAS I installed and are installing the 066-01146-1211 TCAS II
Computer at location options B, C or D.) Install the 9690550 Feed Thru Plate Installation. (Refer to
Cessna Engineering Drawing 9690550.)
G. 9212004-50 Blanking Plate Assembly to replace TCAS I CTL and RMU. (Refer to Cessna
Engineering Drawing 9690575.)